• KSCE Journal of Civil and Environmental Engineering Research
• /
• v.13 no.3
• /
• pp.129-138
• /
• 1993

In this study, the applicability of finite analytic method (FAM) is studied by selecting linearized-Burgers equation and Burgers equation which have convective and diffusive behaviors as the model equation of Navier-Stokes equations and by comparing numerical solution of finite difference method (FDM) and finite analytic method. The results are as follows. It is shown that the convergence of FAM for steady-state analytic solution of linearized-Burgers equation and Burgers equation is better than that of FDM under the same criteria. Also the accuracy of FAM for transient solution of Burgers equation is excellent. Especially, it is shown that oscillation phenomenon due to dispersion errors which occur according to the choice of grid size in FDM does not occur in FAM at all. So, it can be thought that FAM is numerically very stable scheme, which is free from dispersion errors.

• Journal of KIISE:Information Networking
• /
• v.32 no.2
• /
• pp.244-253
• /
• 2005

In this paper, a performance evaluation model of the switch router with the multiple-buffered crossbar switches is proposed and examined. Buffered switch technique is well known to solve the data collision problem of the crossbar switch. The proposed evaluation model is developed by investigating the transfer patterns of data packets in a switch with output-buffers. The performance of the multiple-buffered crossbar switch is analyzed. Steady state probability concept is used to simplify the analyzing processes. Two important parameters of the network performance, throughput and delay, are then evaluated. To validate the proposed analysis model, the simulation is carried out on a network that uses the multiple buffered crossbar switches. Less than $2\%$ differences between analysis and simulation results are observed. It is also shown that the network performance is significantly improved when the small number of buffer spaces is given. However, the throughput elevation is getting reduced and network delay becomes increasing as more buffer spaces are added in a switch.

• Journal of KIISE:Information Networking
• /
• v.29 no.6
• /
• pp.738-748
• /
• 2002

In this paper, a performance evaluation model of the Multistage Interconnection Network(MIN) with the multiple-buffered crossbar switches is Proposed and examined. Buffered switch technique is well known to solve the data collision problem of the MIN. The proposed evaluation model is developed by investigating the transfer patterns of data packets in a switch with output-buffers. The performance of the multiple-buffered${\alpha}{\times}{\alpha}$ crossbar switch is analyzed. Steady state probability concept is used to simplify the analyzing processes, Two important parameters of the network performance, throughput and delay, are then evaluated, To validate the proposed analysis model, the simulation is carried out on a Baseline network that uses the multiple buffered crossbar switches. Less than 2% differences between analysis and simulation results are observed. It is also shown that the network performance is significantly improved when the small number of buffer spaces is given. However, the throughput elevation is getting reduced and network delay becomes increasing as more buffer spaces are added in a switch.

• The Journal of Korean Institute of Communications and Information Sciences
• /
• v.18 no.6
• /
• pp.815-823
• /
• 1993

In this paper, the structure of modified multiplication-free adaptive filter(M-MADF) and convergence analysis are presented. To evaluate the performance of proposed M-MADF algorithm, fractionally spaced equalizer (FSE) is used. The input signals are quantized using DPCM and the reference signals is processed using a first-order linear prediction filter, and the outputs are processed by a conventional adaptive filter. The filter coefficients are updated using the Sign algorithm. Under the assumption that the primary and reference signals are zero mean, wide-sense stationary and Gaussian, theoretical results for the coefficient misalignment vector and its autocorrelation matrix of the filter are driven. The convergence properties of Sign. MADF and M-MADF algorithm for updating of the coefficients of a digital filter of the fractionally spaced equalizer (FSE) are investigated and compared with one another. The convergence properties are characterized by the steady state error and the convergence speed. It is shown that the convergence speed of M-MADF is almost same as Sign algorithm and is faster that MADF in the condition of same steady error. Especially it is very useful for high correlated signals.

• Proceedings of the Korea Water Resources Association Conference
• /
• 2004.05b
• /
• pp.537-542
• /
• 2004

오염물질의 이송${\cdot}$확산 과정을 해석하기 위하여 계산효율이 높은 3차원 퍼프모형을 개발하였다. 본 연구에서 개발된 퍼프모형은 추적방법에 따라 전방추적모형과 후방추적모형으로 나눌 수 있으며, 이 두 가지 추적방법은 계산효율과 수치오차에 있어서 상이한 특성을 나타내었다. 전방추적 퍼프모형은 일정한 시간간격을 가지므로 정상상태의 연속오염원의 경우에 각각의 퍼프들이 동일한 질량을 갖는다. 그러므로 전방추적 퍼프 모형은 각 퍼프들간의 중첩정도가 일정하지 않다. 이에 관한 오차분석을 수행하기 위하여 본 연구에서는 무차원 퍼프중첩계수를 정의하였다. 퍼프중첩계수란 퍼프의 크기에 대하여 퍼프중심간의 거리가 떨어진 정도를 나타내는 무차원수로서 너무 작은 경우에는 정확도가 떨어지고 너무 큰 경우에는 계산효율이 감소한다. 전방 추적 퍼프모형의 경우, 중첩계수가 작은 초기구간에는 정확도가 떨어지며, 시간이 지남에 따라 중첩계수가 필요이상으로 증가하여 계산효율이 떨어지는 것으로 나타났다. 이에 비해 일정한 중첩정도를 갖는 후방추적 퍼프모형의 경우에는 전 영역에 걸쳐서 정확도와 계산효율이 높은 것으로 나타났다. 하지만 일정한 시간간격 마다 농도장을 계산하고자 할 때, 전방추적법은 단 한번의 전체계산을 통하여 수행가능하지만 후방추적법의 경우에는 매 출력시간마다 초기시점까지 반복해서 계산해야하는 단점이 있다. 경계처리에 있어서 입자추적모형과 상이한 방법을 사용하는 퍼프모형은 폐경계에서는 입자추적모형과 동일한 결과를 나타내지만 개경계에서는 다른 결과를 나타내었다. 또한 오염원이 임의의 공간적 분포를 갖는 경우, 퍼프모형은 입자추적모형보다는 적은 수의 퍼프를 사용할 수 있지만 이에 따른 경계면에서의 수치오차를 발생하였다. 본 연구에서는 개발된 퍼프모형을 검증하고 장${\cdot}$단점을 분석하기 위하여 흐름이 일정한 경우와 전단흐름의 경우에 대하여 이송${\cdot}$확산 수치모의를 수행하였으면, 이를 각각의 경우의 해석해 결과와 비교${\cdot}$분석하였다. 후방추적 퍼프모형은 전방추적 퍼프모형에 비하여 사용된 퍼프수와 관계없이 작은 오차를 발생하였으며, 전체적으로 퍼프 모형이 입자모형보다는 훨씬 적은 수의 계산을 통해서도 작은 오차를 나타낼 수 있다는 것을 알 수 있었다. 그러나 Gaussian 분포를 갖는 퍼프모형은 전단흐름에서의 긴 유선형 농도분포를 모의할 수 없었고, 이에 관한 오차는 전단계수가 증가함에 따라 비선형적으로 증가하였다. 향후, 보다 다양한 흐름영역에서 장${\cdot}$단점 분석 및 오차해석을 수행한 후에 각각의 Lagrangian 모형의 장점만을 갖는 모형결합 방법을 제시할 수 있을 것으로 판단된다.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.30 no.1
• /
• pp.105-113
• /
• 2002

In this study, the steady state performance analysis program was developed for a turboprop engine, and its performance was analyzed at uninstalled and installed conditions. For the purpose of evaluation the developed program was compared with the performance data provided by the engine manufacturer and analysis results of GASTURB8.0 program. It was confirmed that the developed program was reliable because the results by the developed program were well agreed with those by GASTURB8.0 within %%. The linear and non-linear GPA(Gas Path Analysis) programs for performance diagnotics were developed, and selection of optimal measurement variables was studied. Furthermore, in order to investigate effects of the number and the kind of measurement variables, the linear and non-linear GPAs were analyzed with various measurement set. If the measurement parameters were properly selected, the reliable and economic faults detection might be possible even thought the small number of measuring parameters were used.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.31 no.4
• /
• pp.60-68
• /
• 2003

In this study, a steady state performance analysis program was developed for a turbofan engine, and its performance was analyzed at installed conditions. For the purpose of evaluation, the developed program was compared with the performance data provided by the engine manufacturer. It was confirmed that the developed program was reliable because the results by the developed program were well agreed with those by the engine manufacturer within 3.5%. The non-linear GPA(Gas Path Analysis) program for performance diagnostics were developed, and selection of optimal measurement variables was studied. Furthermore, in order to investigate effects of the number and the kind of measurement variables, the non-linear GPA was analyzed with various measurement sets. Finally, the measurement parameters selected in the previous step were applied to the fault detection analysis of the 2-spool separate flow type turbofan engine.

• Journal of the Korean Institute of Illuminating and Electrical Installation Engineers
• /
• v.14 no.5
• /
• pp.27-35
• /
• 2000

This paper deals with a control strategy for constant output power of SSRT(Soft Switching Resonant Type) FB(Full Bridge) DC-DC converter by an improved phase shift controller. When the FB DC-DC converter for the high density and the high effect control is operated in high speed switching, the switching loss and switching stress of the switching devices are increased. So, the soft switching method, which has the phase shift control with the digital I-PD controller, must be use in order to reduce its. And the output voltage that controlled by the digital I-PD controller tracks a reference without steady state error in variable input voltage. The validity of control strategy that proposed is verified from simulation results and experimental results by the DSP(TMS320C32).

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2017.05a
• /
• pp.213-217
• /
• 2017

Since more than 30% of the liquid rocket engine failures occur during the start-up process, and the Space Shuttle Main Engine (SSME) is especially sensitive to small changes in propellant conditions, a 2% error in the valve position or a 0.1sec timing error could lead to significant damage of the engine, simulation modeling of start-up process is important. However, there are many difficulties associated with engine start-up process caused by nonlinear mass flow and heat transfer characteristics associated with filling an unconditioned engine system with cryogenic propellants. In this paper, we modelled a SSME simulation model using partially Computational Fluid Dynamics (CFD) method to solve these problems and checked the performance by comparing with the performance of the simulation model using the lumped method under the state of normal condition.

• Proceedings of the Korean Nuclear Society Conference
• /
• 1995.10a
• /
• pp.396-402
• /
• 1995

영광 3,4호기의 부분충수 운전중 정지냉각계통이 상실되고 가압기 Manway가 개방된 사고에 대하여 RELAP5/MOD3.1.2의 열수력 코드를 이용하여 모의하였다. 계산결과 계통의 압력은 최고 1.74bar 까지 도달하였으며, 사고 발생 후 약 1시간 이후부터 계통은 노심이 노출될 때까지 유사 정상상태를 유지한다. 이때 가압기 Manway를 통해 방출되는 증기량은 약 4 kg/s로 붕괴열의 약 80%를 담당하고 증기발생기 2차측에 의해 나머지 20% 가량 제거된다. 또한 비응축성 가스는 계통에 남아 있는 한 계통의 압력 상승율을 증가시키며, RELAP5/MOD3.1.2 계산결과는 일차계통 전체 냉각재의 약 26 %의 질량오차를 나타냈다.